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  5. § 27.977
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14 CFR · Part 27

14 CFR § 27.977

Fuel tank outlet.

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Read in Subpart E
Part 27 Contents
  • Subpart A: General
  • Subpart B: Flight
  • Subpart C: Strength Requirements
  • Subpart D: Design and Construction
  • Subpart E: Powerplant
  • Subpart F: Equipment
  • Subpart G: Operating Limitations and Information
  • Appendix A to Part 27: Instructions for Continued Airworthiness
  • Appendix B to Part 27: Airworthiness Criteria for Helicopter Instrument Flight
  • Appendix C to Part 27: Criteria for Category A
  • Appendix D to Part 27: HIRF Environments and Equipment HIRF Test Levels
(a)

There must be a fuel stainer for the fuel tank outlet or for the booster pump. This strainer must—

(1)

For reciprocating engine powered rotorcraft, have 8 to 16 meshes per inch; and

(2)

For turbine engine powered rotorcraft, prevent the passage of any object that could restrict fuel flow or damage any fuel system component.

(b)

The clear area of each fuel tank outlet strainer must be at least five times the area of the outlet line.

(c)

The diameter of each strainer must be at least that of the fuel tank outlet.

(d)

Each finger strainer must be accessible for inspection and cleaning.

Reflects the eCFR edition current as of September 29, 2026. Retrieved from ecfr.gov on October 16, 2026.

Primary Source

  • Official Source (14 CFR · Part 27)